Orlando-Intl

The aircraft departed La Isabela-Dr. Joaquín Balaguer Airport on a charter flight to Orlando, carrying six passengers and three crew members. Shortly after takeoff, the crew informed ATC about technical problems and was cleared to divert to Santo Domingo-Las Américas Airport for an emergency landing. On approach, the aircraft went out of control and crashed, bursting into flames. The aircraft disintegrated on impact and all nine occupants were killed, among them the Portorican music artist José Angel Hernández aka Flow La Movie. According to a preliminary report, the crew encountered technical problems with the spoilers and maintenance was performed to change the ground spoiler actuators. After maintenance, the crew completed a ground check and while all spoilers properly deployed on both wings, only the spoilers on the left wing retracted as the spoilers on the right wing remained deployed. The crew failed to notice this asymetry. Immediately after takeoff, the crew reported controllability problems and elected to return but finally decided to divert to Las Américas Airport. The aircraft eventually went out of control and crashed 16 minutes after takeoff.

The airplane had undergone routine maintenance, and was returned to service on the day prior to the incident flight. The mechanics who performed the maintenance did not secure the right engine cowling using the procedure outlined in the airplane's maintenance manual. The mechanic who had been working on the outboard side of the right engine could not remember if he had fastened the three primary outboard cowl fasteners before returning the airplane to service. During the first flight following the maintenance, the right engine's top cowling departed the airplane. The pilot secured the right engine, but the airplane was unable to maintain altitude, so he then identified a forced landing site. The airplane did not have a sufficient glidepath to clear a tree line and buildings, so he landed the airplane in a clear area about 1,500 yards short of the intended landing area. The airplane came to rest in a field of scrub brush, and about 5 minutes after the pilot deplaned, the grass under the left engine ignited. The subsequent brush fire consumed the airplane. Examination of the right engine cowling revealed that the outboard latching fasteners were set to the "open" position. When asked about the security of the cowling during the preflight inspection, the pilot stated that he "just missed it."

On October 25, 1999, about 1213 central daylight time (CDT), a Learjet Model 35, N47BA, operated by Sunjet Aviation, Inc., of Sanford, Florida, crashed near Aberdeen, South Dakota. The airplane departed Orlando, Florida, for Dallas, Texas, about 0920 eastern daylight time (EDT). Radio contact with the flight was lost north of Gainesville, Florida, after air traffic control (ATC) cleared the airplane to flight level (FL) 390. The airplane was intercepted by several U.S. Air Force (USAF) and Air National Guard (ANG) aircraft as it proceeded northwestbound. The military pilots in a position to observe the accident airplane at close range stated (in interviews or via radio transmissions) that the forward windshields of the Learjet seemed to be frosted or covered with condensation. The military pilots could not see into the cabin. They did not observe any structural anomaly or other unusual condition. The military pilots observed the airplane depart controlled flight and spiral to the ground, impacting an open field. All occupants on board the airplane (the captain, first officer, and four passengers) were killed, and the airplane was destroyed.
Crew:
Michael Kling,
Stephanie Bellegarrigue.
Passengers:
Payne Stewart,
Van Ardan,
Bruce Borland,
Robert Fraley.

During landing roll, the airplanes normal braking system failed as a result of hydraulic fluid leak(s). At the pilot's request, deployment of the drag chute and application of the emergency braking system was performed by the first officer. According to the first officer, application of the emergency brakes caused the airplane to yaw. The first officer then pulled up on the emergency brakes handle followed by re-application of braking pressure. This action took place several times during the landing roll. Gates' Learjet Flight Training Manual (Page 105) states, 'In using the emergency brake lever, slow steady downward pressure is required. Each time the lever is allowed to return upward to the normal position, nitrogen is evacuated overboard. Brace your hand so you will not allow the lever to move up and down inadvertently on a bumpy runway.' The airplane overran the end of the runway and collided with the Instrument Landing System back course antennae.

The pilot/owner and a flight instructor had flown in to pick-up passengers. The owner was not multiengine rated and was receiving instruction from the instructor. The airplane was fueled and two adults and three children were boarded about 1 hour later. The owner was the flying pilot in the left seat. The owner stated that the 4,500 foot long runway was covered with 2 1/2 to 3 inches of snow and slush. He further stated that during the takeoff roll, 'The snow was so bad we could not get off the ground...' The pilot estimated that he aborted the takeoff at 100 mph, the braking action was zero, and the airplane went off the end of the runway. According to a witness, the five passengers arrived with 'lots of heavy bags.' After the accident, the baggage was removed before it could be weighed. An estimated airplane takeoff weight of 7,856 pounds was computed without baggage, based upon weights from the airplane weight and balance form, the police report, and FAA records. According to the Pilot's Operating Handbook, the maximum takeoff weight was published at 7,560 pounds.

En route from Orlando to Cancún, the crew got lost and was unable to follow the prescribed route, causing the aircraft to deviate from the flight plan to the west. Eventually, the crew was vectored to the Tampico-General Francisco Javier Mina Airport located about 1,144 km northwest of the destination airport. On final approach, both engines failed simultaneously due to fuel exhaustion. The aircraft lost speed, stalled and collided with ILS equipment located about 300 metres short of runway 31. Upon impact, the undercarriage were sheared off and the aircraft crash landed on the runway and came to rest 220 metres further. All 47 occupants evacuated safely while the aircraft was damaged beyond repair.

On August 28, 1995, about 1331 eastern daylight time, a Beech E18S, N171LG, registered to Caribbean Leasing Company, and operated by Avmac Air, Inc., as a 14 CFR Part 135 nonscheduled international cargo flight, from Orlando, Florida, to Freeport, Bahamas, crashed into the Atlantic Ocean, about 45 miles northwest of Freeport. Instrument meteorological conditions prevailed at the time and an instrument flight rules flight plan was filed. The aircraft was destroyed. The airline transport-rated pilot has not been located and is presumed to have been fatally injured. The flight originated from Orlando, on August 28, 1995, about 1229. A person identifying himself as the pilot of N171LG contacted the FAA Miami Flight Service Station by radio at 1328:33. The pilot reported he was 46 miles northwest of Freeport and requested information on the weather at Freeport. The pilot was given the weather. At 1330:15 the pilot reported he had an emergency. The controller asked what is the emergency and the pilot reported "fire onboard." No further transmissions from the flight were received and attempts to contact the flight were unsuccessful. See the transcript of communications. Search and rescue efforts were initiated and at 1600, a oil slick, the left main landing gear from N171LG, and personal effects of the pilot and debris from the cabin contents were found floating on the ocean surface, 40 miles northwest of Freeport. Examination of the recovered debris showed no evidence of fire damage. The main wreckage of N171LG was not located and recovered.

The pilot was cleared for takeoff on an IFR flight. After takeoff, the pilot did not contact departure control. A search was initiated and the aircraft was found near the departure end of runway 07. There was evidence the aircraft had impacted in a left wing down, nose low attitude. No preimpact part failure or malfunction of the aircraft was found. Both occupants were killed.